发明名称 MICRO UNMANNED AERIAL VEHICLE AND METHOD OF CONTROL THEREFOR
摘要 A micro unmanned aerial vehicle or drone (“UAV”) 10 is remotely controlled through an HMI, although this remote control is supplemented by and selectively suppressed by an on-board controller. The controller operates to control the generation of a sonar bubble that generally encapsulates the UAV. The sonar bubble, which may be ultrasonic in nature, is produced by a multiplicity of sonar lobes generated by specific sonar emitters associated with each axis of movement for the UAV. The emitters produce individual and beamformed sonar lobes that partially overlap to provide stereo or bioptic data in the form of individual echo responses detected by axis-specific sonar detectors. In this way, the on-board controller is able to interpret and then generate 3-D spatial imaging of the physical environment in which the UAV is currently moving or positioned. The controller is therefore able to plot relative and absolute movement of the UAV through the 3-D space by recording measurements from on-board gyroscopes, magnetometers and accelerometers. Data from the sonar bubble can therefore both proactively prevent collisions with objects by imposing a corrective instruction to rotors and other flight control system and can also assess and compensate for sensor drift.
申请公布号 EP2909689(B1) 申请公布日期 2016.10.05
申请号 EP20130785582 申请日期 2013.10.22
申请人 BCB INTERNATIONAL LIMITED;TORQUING GROUP LTD. 发明人 REEDMAN, IVAN;DAVIES, BARRY
分类号 G05D1/10 主分类号 G05D1/10
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